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EP0070480B1 - Method and apparatus for positioning the pressure plate in material testing devices - Google Patents

Method and apparatus for positioning the pressure plate in material testing devices Download PDF

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Publication number
EP0070480B1
EP0070480B1 EP19820106183 EP82106183A EP0070480B1 EP 0070480 B1 EP0070480 B1 EP 0070480B1 EP 19820106183 EP19820106183 EP 19820106183 EP 82106183 A EP82106183 A EP 82106183A EP 0070480 B1 EP0070480 B1 EP 0070480B1
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EP
European Patent Office
Prior art keywords
spherical
support
sleeve
carrier
cup
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
EP19820106183
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German (de)
French (fr)
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EP0070480A2 (en
EP0070480A3 (en
Inventor
Harald A. Solmitz
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Individual
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Individual
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Filing date
Publication date
Priority claimed from DE19813128394 external-priority patent/DE3128394C2/en
Priority claimed from DE19823201389 external-priority patent/DE3201389A1/en
Application filed by Individual filed Critical Individual
Publication of EP0070480A2 publication Critical patent/EP0070480A2/en
Publication of EP0070480A3 publication Critical patent/EP0070480A3/en
Application granted granted Critical
Publication of EP0070480B1 publication Critical patent/EP0070480B1/en
Expired legal-status Critical Current

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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N3/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N3/02Details
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/0014Type of force applied
    • G01N2203/0016Tensile or compressive
    • G01N2203/0019Compressive
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/02Details not specific for a particular testing method
    • G01N2203/04Chucks, fixtures, jaws, holders or anvils
    • G01N2203/0405Features allowing alignment between specimen and chucks

Definitions

  • the sample surfaces that come into contact with the pressure plates are rarely parallel to one another.
  • One of the pressure plates preferably the upper pressure plate, must therefore be able to adapt to the inclination of the upper sample surface. It is therefore customary to spherically support the upper pressure plate with a spherical cap and spherical shell.
  • the paddle In order to achieve a perfect adaptation of the inclination of the pressure plate to the inclination of the sample surface when setting up, the paddle must be inclined almost without force relative to the bowl, which practically requires a frictionless contact of the surfaces.
  • the upper pressure plate should remain in the position in which it was set when setting it up in order to have a clear and reproducible test condition, since when tipping movements are permitted during loading, it is difficult or impossible to make comparable statements about the application of force can. A very large amount of friction between the contact surfaces is necessary to maintain this condition.
  • a testing machine is known in which a pressure plate is designed in the form of a hemisphere mounted in a spherical shell.
  • the hemisphere has a spigot that passes through a central opening in the spherical shell and is pressed against the spherical shell by a spring acting on the end of the spigot.
  • the pressure plate Due to the spherical mounting, the pressure plate should be adjustable at a limited angle to the inclination of the surface of the sample. After the adjustment, the pressure plate is to be locked by a locking device acting at the end of the pin.
  • the entire contact surface of the spherical shell and spherical cap remains engaged in the usual way, both during adjustment and during testing, so that, for example, the known difficulties arise when adjusting to the inclination of the sample surface.
  • the object of the invention is to provide a method for a printing plate storage and an apparatus for performing the method, which make it possible in a simple and economical manner to meet the requirement for easy adjustability when setting up the printing plate and immobility of the printing plate during the further course of the experiment.
  • the mounting of the spherical cap and spherical shell is divided into two mechanical states which follow one another in time, namely in the first state, in which, while maintaining a force-fitting centering of the spherical cap relative to the shell, the pressure plate is adjusted to the inclination of those driven against it with almost no force Pressure area of the sample takes place and the further state in which a relative movement of the calotte in the shell is prevented.
  • the spherical shell is supported in relation to the calotte by one or more partial surfaces, the surfaces of which are characterized by very good sliding properties, the arrangement of these partial surfaces in or near the center of the calotte favoring easy adjustment and following these partial surfaces acting as supporting surfaces Exceeding a low preload are pushed back, whereby a system occurs on the second partial area, which corresponds approximately to the entire contact area between the calotte and the shell, both or one of the contact areas having partially or completely greater frictional resistances.
  • the kinematics of the tilting movement are selected differently for the two states, the center of the radius of the spherical shell being in the plane of the pressure surface of the pressure plate in the first phase, the set-up phase, and thereby a favorable attack of the adjusting forces being achieved and when the sample and pressure plate come into contact, there are no horizontal frictional resistances that counteract the tilting movement.
  • the center of the radius of the spherical shell lies below the pressure surface of the pressure plate, which additionally counteracts horizontal frictional forces when the plate is adjusted.
  • the form fit between the calotte and the support is brought about by displaceable support elements which are loaded by spring force or hydraulic pressure and which support the calotte against the shell, the end faces of the support elements being made of a material with very good sliding properties or coated with it.
  • the second phase at At the beginning of the actual pressure test, the counter load of the spring force or hydraulic pressure acting on the support elements is overcome by the test load, the support elements recede and the calotte and the shell come into direct contact on almost all of their contact surfaces.
  • the surface of one of the two parts is produced with a higher roughness, namely the part in which the support elements are installed.
  • the counter surface can additionally have a greater degree of roughness on the surfaces on which the end faces of the support bolts or bushings are not in contact.
  • test conditions the test conditions, the dimensions of the sample and the pressure plate, it may be advantageous and desirable to be able to change the resistance of the pressure plate to a change in inclination in order to create optimal conditions in the alignment phase and the test phase.
  • the setting torque exerted by the sample on the pressure plate is in fact different in size.
  • an assumed size e.g. B. the pressure plate diagonal and the spherical shell radius R
  • the setting torque exerted by the inclined sample surface is small when the sample diagonal is small compared to the two device dimensions above, whereas the setting torque is larger when the sample diagonal is larger than the above device dimensions, in particular larger than the spherical shell radius.
  • the resistance that counteracts the adjustment of the pressure plate should be as small as possible when testing a sample with a small diagonal, whereas when examining a sample with a large diagonal, especially with longer ones Rerchtechamples the stall resistance should be larger to avoid unstable conditions.
  • the change in the setting resistance is achieved in that the resistance of the pressure plate to a change in its inclination is set by adjusting a prestressing force acting on the contact surfaces and / or the ratio of the prestressing forces acting on the contact surfaces.
  • hydraulic biasing devices are preferably used, which combined with biasing springs, for. B. steel springs, or work without such springs.
  • the prestressing devices can either be installed in the spherical cap or on the side of the spherical shell or partly in the spherical cap, partly on the side of the spherical shell.
  • the support bushes can be withdrawn during the test phase and have no contact with the counter surface or they can remain applied with a possibly constant tension of the preload spring or the pressure in the hydraulic chamber and act as a recoil damper when the pressure plate springs back after the specimen break.
  • FIG. 1 a shows the embodiment of the subject of the invention on a pressure plate 3 suspended by a support or center bolt 4.
  • a support sleeve 14 which can be displaced in the axial direction, the upper end face 15 of which has a surface with good sliding properties, e.g. B. plastic coating.
  • the spring 5 By tightening the spring 5, by the nut 6, the support sleeve with attached pressure plate is raised so far that the end face 15 of the support sleeve 14 rests against the ball socket 1 with low pressure.
  • the spherical cap and pressure plate rest on the outer shoulder 10 of the support sleeve, which is braced against the supporting bolt 4 by the biasing spring 11.
  • the same arrangement is shown in FIG. 1b, but with hydraulic recoil damping.
  • the annular chamber 24 is connected during the loading process via the pressure line 22 to a hydraulic accumulator which has a constant pressure level.
  • the pressure level required for damping can further tension the preload spring 11 and thus press the spherical cap against the spherical shell, while at the same time the support sleeve 14 can be pushed down until it disappears under the spherical surface, during the setting process the annular chamber can be depressurized be.
  • the spherical cap is supported and aligned by at least three support bolts 9 which slide in bores of the spherical cap and are preloaded with springs 11. The springs are supported against the pressure plate 3.
  • Similar support bolts 9 are present in the embodiment according to FIG. 2 b.
  • the bias spring 11 is supported against an end plate 12, for. B. from a Seeger ring.
  • Sliders 25 made of a slightly sliding material are inserted into the end face of the support bolts.
  • the pressure plate plane 16 moves upward from the center A of the shell radius R under load.
  • the contact surface of the supporting bolt 4 with a small spherical cap 8 against the small spherical shell 7 is brought up to the center of the spherical cap 2 in order to keep the setting forces for the pressure plate 3 low.
  • 3 a shows the embodiment of the subject matter of the invention on a pressure plate which is suspended from at least three springs 27 which engage on the outer edge of the pressure plate 3.
  • a support sleeve 14 is installed in the center, the shoulder of which is pressed by the spring 11 against the shoulder 10 of the bore in the spherical cap 2.
  • three support bolts 9 are arranged parallel to the machine axis in the spherical cap.
  • the bias of the spring 11 can be adjusted with the screw.
  • a support pin 9 which is arranged in the central bore of the spherical shell 1 and which is loaded by the spring 11, is provided.
  • At least three support bolts 9 are arranged radially in the spherical shell.
  • the guide bore which is open at the top, is closed by a screw 18, which serves to bias the spring 11.
  • the pretension for the support bolts or bushes is built up hydraulically.
  • the support pin 9 is connected to a piston 17 with sealing rings 17a, which slides in a bore in the calotte. The back of the bore is closed with sealing rings by a sealing plug 18.
  • the pressure oil is supplied through line 23.
  • the support element is arranged in the spherical shell 1, the bore for guiding the support bolt 9 and the pressure piston 17 is incorporated from above and closed with a threaded plug 18 with a connection bore 22 for the pressure line.
  • the hydraulic support elements described above are connected to a pressure accumulator with constant oil pressure or they are supplied by a feed pump.
  • the feed pump feeds into the support elements via a pressure regulator and a check valve connected behind it.
  • a pressure relief valve is attached to the support element.
  • the end faces of the support bushes or support bolts, which are built into the spherical shell, have a shape adapted to the spherical shell, FIG. 2 a), or are spherical (FIG. 3 b).
  • the end face of the support bolts and bushings, which are installed in the spherical shell 1, have a shape adapted to the spherical shell or spherical or a flat shape (Fig. 4b).
  • Fig. 8 shows the execution of the subject matter of an arrangement in which two hydraulic clamping devices are used, which are installed in the spherical cap 2, and which can work independently of each other.
  • a support spring z. B. coil spring can be dispensed with.
  • the prestress for the abutment of the end face 15 of the support bush 14 against the spherical shell 1 in the set-up phase is brought about by the pressure chamber 24.
  • the bearing of the spherical cap after the end of the adjustment phase on the spherical shell is brought about by the carrying sleeve 28 with the pressure chamber 24a.
  • the pressure chamber 24a can be depressurized and the pressure chamber 24 can be subjected to a pressure which just applies the support sleeve to the ball socket or presses it with a higher prestress.
  • the test specimen and the pressure plate can be replaced by the z. B.
  • the hydraulic drive of the machine located underneath can be raised until the spherical cap rests on the spherical shell and then a preload is generated via the annular chamber 24a: however, the pressure plate can also first be raised via the annular chamber 24a and pressed against the spherical shell before the hydraulic drive the machine lifts the sample.
  • the annular chamber 24 can be depressurized, so that the support sleeve can sink behind the surface of the spherical cap.
  • the annular chamber 24a can be under a possibly constant hydraulic pressure and can serve as a shock absorber via the support sleeve when the pressure plate springs back after the sample has broken.
  • the spherical cap itself can be pressed against the spherical shell by the carrying bushing during the test, whereby the usual preload spring can be omitted.
  • FIG. 9 a shows the subject of the invention in an embodiment in which the support sleeve 14 and the support sleeve 28 can both be introduced from one side into the cylindrical bore of the spherical cap.
  • the support sleeve is pressed by the spring 11 against the spherical shell.
  • the contact pressure is set in the annular chamber 24 by the hydraulic force counteracting the spring force.
  • the support sleeve can be retracted behind the calotte surface by the hydraulic pressure in chamber 24.
  • the carrying sleeve 28 has a hydraulic pressure chamber 24a.
  • 9 b shows the subject matter of the invention in an embodiment in which only the support sleeve has a hydraulic drive with a pressure chamber 24.
  • the spring 11 takes effect and the support sleeve emerges from the spherical cap.
  • the support sleeve is first pulled back by an increase in pressure in the chamber 24, then the elongated lower part of the support sleeve settles on the support plate 41 as a stroke limiter 38, the further increase in pressure in the chamber 24 pressing the spherical cap against the spherical shell.
  • the support sleeve 21 and the spring 11 can dampen the recoil when the pressure plate springs back.
  • FIG. 10 shows the subject matter of the invention in an embodiment in which the hydraulic support sleeve 14 and the hydraulic support sleeve 28 are arranged on the side of the spherical shell, the function of the arrangement correspondingly being the same as that described for FIG. 1 .
  • a compression spring 5 can also be installed for the suspension of the pressure plate.
  • a pretensioning device is equipped with a hydraulic system, the other is equipped with a spring, the supporting bolt being connected to the piston 29, which can slide in the cylinder bore 30, and the supporting bush 14 is loaded by the pretensioning spring 11.
  • the pressure chamber 31 is relieved, as a result of which the support sleeve 14 emerges from the spherical cap.
  • the bias spring 11 can be dimensioned independently of the bias in the support bolt.
  • a chamber 32 which can act as recoil vapors, is installed above the piston and can be connected to a pressure relief valve or a pressure accumulator for adjusting the damping effect.
  • the cylinder with piston 29 can also be arranged as a separate element on the surface of the spherical shell cross member, which provides a hydraulic drive.
  • FIG. 12 shows an arrangement with a support sleeve 14, tension spring 11 and hydraulic support sleeve 28.
  • the pressure chamber 24a is relieved, as a result of which the support sleeve comes into contact alone.
  • FIG. 13 there are at least two cylinder bores 34 with plummer pistons 33, which can lift the supporting bolt 4 via a supporting disk 39.
  • the support sleeve 14 is loaded with the spring 11.
  • the plunger pistons can also be arranged in separate cylinders which are arranged on the spherical shell cross member.
  • the support sleeve 14 and the support sleeve 28 are combined in one component (so-called support support sleeve).
  • the pressure chamber 24a can be depressurized, as a result of which the support carrying sleeve 14/28 rests on the shoulder 36 of the spherical shell.
  • the support liner is raised by pressure in the chamber 24 a, whereupon the support liner rests against the shoulder 35 of the support bolt 4 and takes over the prestressing for it.
  • the stroke of the support bushing 14/28 can be designed so that the support bushing only rests against the shoulder 35 of the support bolt 4 when the support bushing has withdrawn behind the surface of the spherical shell.
  • FIG. 15 shows an embodiment in which a spacer sleeve 37 is used instead of the shoulder 35 of FIG. 14.
  • a spring can also replace the spacer sleeve.
  • the method and the device according to the invention provide clear and reproducible test conditions for carrying out printing tests, since both the easy adjustability of the printing plate inclination is achieved in the setting phase and the prevention of relative displacements of the calotte and shell during the actual printing test. To achieve this goal, only a few additional, simple machine elements are required, so that the device can be produced economically.

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Description

Zur Durchführung von Werkstoffprüfungsn ist es bekanntlfch notwendig, daß die Prüfbedingungen in der Prüfmaschine eindeutig und reproduzierbar sind. Bei der Druckprüfung war es bisher schwierig, diese notwendige Bedingung zu erfüllen, dies gilt insbesondere bei der Krafteinleitung über die Druckplatte auf die Probe.In order to carry out material tests, it is known that the test conditions in the testing machine are clear and reproducible. In the pressure test, it was previously difficult to meet this necessary condition, this applies in particular when force is applied to the sample via the pressure plate.

Bei Druckproben sind die mit den Druckplatten in Berührung kommenden Probeflächen selten parallel zueinander. Eine der Druckplatten, bevorzugt die obere Druckplatte, muß sich daher der Neigung der oberen Probefläche anpassen können. Es ist daher üblich, die obere Druckplatte sphärisch durch Kugelkalotte und Kugelschale zu lagern. Um eine einwandfreie Anpassung der Neigung der Druckplatte an die Neigung der Probenoberfläche beim Einrichten zu erreichen, muß sich die Katotte gegenüber der Schale nahezu kraftlos neigen lassen, was praktisch einen reibungsfreien Kontakt der Flächen voraussetzt. Andererseits soll während des Versuches die obere Druckplatte in der Stellung verharren, in die sie beim Einrichten eingestellt wurde, um eine eindeutige und reproduzierbare Prüfbedingung zu haben, da bei Zulassung von Kippbewegungen während der Belastung schwer oder gar nicht seindeutig vergleichbare Aussagen über die Krafteinleitung gemacht werden können. Zur Einhaltung dieser Bedingung ist eine sehr große Reibung zwischen den Kontaktflächen notwendig.In the case of pressure samples, the sample surfaces that come into contact with the pressure plates are rarely parallel to one another. One of the pressure plates, preferably the upper pressure plate, must therefore be able to adapt to the inclination of the upper sample surface. It is therefore customary to spherically support the upper pressure plate with a spherical cap and spherical shell. In order to achieve a perfect adaptation of the inclination of the pressure plate to the inclination of the sample surface when setting up, the paddle must be inclined almost without force relative to the bowl, which practically requires a frictionless contact of the surfaces. On the other hand, during the test, the upper pressure plate should remain in the position in which it was set when setting it up in order to have a clear and reproducible test condition, since when tipping movements are permitted during loading, it is difficult or impossible to make comparable statements about the application of force can. A very large amount of friction between the contact surfaces is necessary to maintain this condition.

Diese gegensätzlichen Forderungen des Einstellens der Druckplattenneigung beim Einrichten ohne merklichen Widerstand und der praktisch unbeweglichen Druckplatte während des Versuches sind mit den bisher bekannten bzw. üblichen Maßnahmen nicht zu erfüllen.These conflicting requirements of setting the pressure plate inclination when setting up without noticeable resistance and the practically immovable pressure plate during the test cannot be met with the previously known or customary measures.

Aus der US-A-3 545 263 (entsprechend DE-OS 19 03 042) ist eine Prüfmaschine bekannt, bei der eine Druckplatte in Form einer in einer Kugelschale gelagerten Halbkugel ausgebildet ist. Die Halbkugel weist einen durch eine mittige Öffnung in der Kugelschale gehenden Zapfen auf und wird durch eine am Zapfenende angreifende Feder gegen die Kugelschale gedrückt. Durch die kugelige Lagerung soll die Druckplatte in einem begrenzten Winkel auf die Neigung der Oberfläche der Probe einstellbar sein. Nach der Einstellung soll die Druckplatte durch eine am Zapfenende wirkende Feststellvorrichtung arretiert werden. Bei dieser Ausführung bleibt in üblicher Weise sowohl bei der Einstellung als auch bei der Prüfung die gesamte Berührungsfläche von Kugelschale und Kugelkalotte im Eingriff, so daß beispielsweise bei der Einstellung auf die Neigung der Probenoberfläche die bekannten Schwierigkeiten auftreten.From US-A-3 545 263 (corresponding to DE-OS 19 03 042) a testing machine is known in which a pressure plate is designed in the form of a hemisphere mounted in a spherical shell. The hemisphere has a spigot that passes through a central opening in the spherical shell and is pressed against the spherical shell by a spring acting on the end of the spigot. Due to the spherical mounting, the pressure plate should be adjustable at a limited angle to the inclination of the surface of the sample. After the adjustment, the pressure plate is to be locked by a locking device acting at the end of the pin. In this embodiment, the entire contact surface of the spherical shell and spherical cap remains engaged in the usual way, both during adjustment and during testing, so that, for example, the known difficulties arise when adjusting to the inclination of the sample surface.

Aufgabe der Erfindung ist es, ein Verfahren für eine Druckplattenlagerung und eine Vorrichtung zur Durchführung des Verfahrens zu schaffen, die es auf einfache und wirtschaftliche Weise ermöglichen, die Forderung nach leichter Einstellbarkeit beim Einrichten der Druckplatte und Unbeweglichkeit der Druckplatte während des weiteren Versuchsablaufs zu verwirklichen.The object of the invention is to provide a method for a printing plate storage and an apparatus for performing the method, which make it possible in a simple and economical manner to meet the requirement for easy adjustability when setting up the printing plate and immobility of the printing plate during the further course of the experiment.

Diese Aufgabe wird durch die in den Patentansprüchen 1 und 7 angegebenen Merkmale gelöst. Die weiteren Ansprüche betreffen Ausgestaltungen der Erfindung.This object is achieved by the features specified in claims 1 and 7. The further claims relate to configurations of the invention.

Nach der Erfindung wird die Lagerung der Kugelkalotte und Kugelschale in zwei, sich zeitlich folgende, mechanische Zustände aufgeteilt, nämlich in den ersten Zustand, bei dem unter Einhaltung einer kraftschlüssigen Zentrierung der Kalotte zur Schale ein nahezu kraftloses Einstellen der Druckplatte auf die Neigung der dagegen gefahrenen Druckfläche der Probe erfolgt und den weiteren Zustand, bei dem eine Relativbewegung der Kalotte in der Schale verhindert wird.According to the invention, the mounting of the spherical cap and spherical shell is divided into two mechanical states which follow one another in time, namely in the first state, in which, while maintaining a force-fitting centering of the spherical cap relative to the shell, the pressure plate is adjusted to the inclination of those driven against it with almost no force Pressure area of the sample takes place and the further state in which a relative movement of the calotte in the shell is prevented.

Hierzu werden für die beiden Funktionen zwei unterschiedliche Berührungsflächen benutzt und wahlweise zusätzlich unterschiedliche kinematische Verhältnisse für den Angriff der Verstellkräfte geschaffen.For this purpose, two different contact surfaces are used for the two functions and, alternatively, different kinematic conditions are created for the attack of the adjusting forces.

Es wird zu Beginn des Versuchs die Kugelschale gegenüber der Kalotte durch eine oder mehrere Teilflächen abgestützt, deren Oberflächen durch sehr gute Gleiteigeschaften gekennzeichnet sind, wobei die Anordnung dieser Teilflächen in oder nähe der Mitte der Kalotte eine leichte Verstellung begünstigen und diese als Stützflächen wirkenden Teilflächen nach Überschreiten einer geringen Vorlast zurückgeschoben werden, wodurch eine Anlage auf der zweiten Teilfläche eintritt, die annähernd der ganzen Berührungsfläche zwischen Kalotte und Schale entspricht, wobei beide oder eine der Berührungsflächen ganz oder teilweise größere Reibwiderstände besitzen.At the beginning of the experiment, the spherical shell is supported in relation to the calotte by one or more partial surfaces, the surfaces of which are characterized by very good sliding properties, the arrangement of these partial surfaces in or near the center of the calotte favoring easy adjustment and following these partial surfaces acting as supporting surfaces Exceeding a low preload are pushed back, whereby a system occurs on the second partial area, which corresponds approximately to the entire contact area between the calotte and the shell, both or one of the contact areas having partially or completely greater frictional resistances.

Eine weiters Maßnahme besteht darin, daß die Kinematik der Kippbswegung für die beiden Zustände unterschiedlich gewählt wird, wobei in der ersten Phase, der Einrichtungsphase, der Mittelpunkt des Radius der Kugelschale in der Druckflächenebene der Druckplatte liegt, und dadurch ein günstiger Angriff der Verstellkräfte erreicht wird und bei der Berührung von Probe und Druckplatte keine horizontalen Reibwiderstände auftreten, die der Kippbewegung entgegenwirken. In der zweiten Phase während der Belastung der Probe liegt dagegen der Mittelpunkt des Radius der Kugelschale unterhalb der Druckfläche der Druckplatte, wodurch der Verstellung der Platte zusätzlich horizontale Reibkräfte entgegenwirken.Another measure is that the kinematics of the tilting movement are selected differently for the two states, the center of the radius of the spherical shell being in the plane of the pressure surface of the pressure plate in the first phase, the set-up phase, and thereby a favorable attack of the adjusting forces being achieved and when the sample and pressure plate come into contact, there are no horizontal frictional resistances that counteract the tilting movement. In the second phase while the sample is loaded, however, the center of the radius of the spherical shell lies below the pressure surface of the pressure plate, which additionally counteracts horizontal frictional forces when the plate is adjusted.

In der ersten Phase, nämlich der Einrichtphase, wird der Formschluß zwischen Kalotte und Abstützung durch verschiebbare Stützelemente bewirkt, die durch Federkraft oder hydraulischen Druck belastet sind und die Kalotte gegen die Schale abstützen, wobei die Stirnflächen der Stützelemente aus einem Werkstoff mit sehr guten Gleiteiganschaften bestehen oder damit beschichtet sind. In der zweiten Phase, bei Beginn des eigentlichen Druckversuchs, wird durch die Prüflast der Gegendruck der Federkraft oder des hydraulischen Druckes, die auf die Stützelemente wirken, überwunden, die Stützelemente treten zurück und die Kalotte und die Schale bekommen nahezu auf ihren ganzen Berührungsflächen direkt Kontakt. Um den Bewegungswiderstand zwischen den beiden Teilen zu erhöhen, wird die Oberfläche einer der beiden Teile mit einer höheren Rauhigkeit hergestellt, und zwar der Teil, in dem die Stützelemente eingebaut sind. Die Gegenfläche kann zusätzlich an den Flächen, auf denen die Stirnflächen der Stützbolzen oder -büchsen nicht anliegen, einen größeren Rauhigkeitsgrad erhalten.In the first phase, namely the set-up phase, the form fit between the calotte and the support is brought about by displaceable support elements which are loaded by spring force or hydraulic pressure and which support the calotte against the shell, the end faces of the support elements being made of a material with very good sliding properties or coated with it. In the second phase, at At the beginning of the actual pressure test, the counter load of the spring force or hydraulic pressure acting on the support elements is overcome by the test load, the support elements recede and the calotte and the shell come into direct contact on almost all of their contact surfaces. In order to increase the resistance to movement between the two parts, the surface of one of the two parts is produced with a higher roughness, namely the part in which the support elements are installed. The counter surface can additionally have a greater degree of roughness on the surfaces on which the end faces of the support bolts or bushings are not in contact.

Beim Zurücktreten der Stützelemente verschiebt sich die Druckfläche der Druckplatte vom Mittelpunkt des Schalenradius fort zur Schale hin, wodurch der Mittelpunkt dann unterhalb der Druckfläche liegt.When the support elements withdraw, the pressure surface of the pressure plate moves away from the center of the shell radius to the shell, as a result of which the center point then lies below the pressure surface.

In Abhängigkeit von der Art des Versuches, den Versuchsbedingungen, den Dimensionen der Probe und der Druckplatte, kann es vorteilhaft und wünschenswert sein, den Widerstand der Druckplatte gegenüber einer Neigungsänderung ändern zu können, um optimale Verhältnisse in der Ausrichtphase und der Versuchsphase zu schaffen.Depending on the type of test, the test conditions, the dimensions of the sample and the pressure plate, it may be advantageous and desirable to be able to change the resistance of the pressure plate to a change in inclination in order to create optimal conditions in the alignment phase and the test phase.

Das von der Probe auf die Druckplatte ausgeübte Einstellmoment ist nämlich von unterschiedlicher Größe. Bei einer angenommenen Größe, z. B. der Druckplattendiagonale und des Kugelschalenradius R, ist das von der geneigten Probenoberfläche ausgeübte Einstellmoment klein, wenn die Probendiagonale klein gegenüber den beiden obigen Gerätemaßen ist, wogegen das Einstellmoment im Verhältnis hierzu größer ist, wenn die Probendiagonale größer als die obigen Gerätemaße ist, insbesondere größer als der Kugelschalenradius.The setting torque exerted by the sample on the pressure plate is in fact different in size. With an assumed size, e.g. B. the pressure plate diagonal and the spherical shell radius R, the setting torque exerted by the inclined sample surface is small when the sample diagonal is small compared to the two device dimensions above, whereas the setting torque is larger when the sample diagonal is larger than the above device dimensions, in particular larger than the spherical shell radius.

Um ein sicheres Einstellen der Druckplatte zu gewährleisten, soll daher, wenn auf einer Prüfmaschine eine Probe mit kleiner Diagonale untersucht werden soil, der Widerstand, der dem Einsteilen der Druckplatte entgegenwirkt, möglichst klein sein, wogegen bei Untersuchungen einer Probe mit großer Diagonale insbesondere bei längeren Rerchtechproben der Einstallwiderstand größer sein sollte, um labile Verhältnisse zu vermeiden.In order to ensure a safe setting of the pressure plate, the resistance that counteracts the adjustment of the pressure plate should be as small as possible when testing a sample with a small diagonal, whereas when examining a sample with a large diagonal, especially with longer ones Rerchtechamples the stall resistance should be larger to avoid unstable conditions.

Nach einer Weiterbildung der Erfindung wird die Anderung des Einstellwiderstandes dadurch erreicht, daß der Widerstand der Druckplatte gegenüber einer Änderung ihrer Neigung dadurch eingestellt wird, daß eine auf die Berührungsflächen wirkende Vorspannkraft und/oder das Verhältnis der auf die Berührungsflächen wirkenden Vorspannkräfte eingestellt wird.According to a further development of the invention, the change in the setting resistance is achieved in that the resistance of the pressure plate to a change in its inclination is set by adjusting a prestressing force acting on the contact surfaces and / or the ratio of the prestressing forces acting on the contact surfaces.

Hierzu werden bevorzugt hydraulische Vorspanneinrichtungen benutzt, die kombiniert mit Vorspannfedern, z. B. Stahlfedern, oder auch ohne solche Federn arbeiten. Die Vorspanneinrichtungen können entweder in der Kugelkalotte oder auf der Seite der Kugelschale oder auch teils in der Kugelkalotte, teils auf der Seite der Kugelschale eingebaut sein.For this purpose, hydraulic biasing devices are preferably used, which combined with biasing springs, for. B. steel springs, or work without such springs. The prestressing devices can either be installed in the spherical cap or on the side of the spherical shell or partly in the spherical cap, partly on the side of the spherical shell.

Die Stützbüchsen können während der Versuchsphase zurückgezogen sein und keinen Kontakt mit der Gegenfläche haben oder sie können mit einer gegebenenfalls konstanten Spannung der Vorspannfeder oder des Drucks in der hydraulischen Kammer angelegt bieiben und als Rückstoßdämpfer bei der Rückfederung der Druckplatte nach dem Probenbruch arbeiten.The support bushes can be withdrawn during the test phase and have no contact with the counter surface or they can remain applied with a possibly constant tension of the preload spring or the pressure in the hydraulic chamber and act as a recoil damper when the pressure plate springs back after the specimen break.

Die Erfindung wird nun an Hand von Zeichnungen, die bevorzugte Ausführungsformen darstellen, weiterhin erläutert.The invention will now be further explained with the aid of drawings which represent preferred embodiments.

Es zeigen:

  • Fig. 1 a Druckplatte mit Mittelbolzenaufhängung und zentraler Stützbüchse
  • Fig 1 b Druckplatte mit Mittelbolzenaufhängung und zentraler Stützbüches für die Rückstoßdämpfung.
  • Fig 2 a Druckplatte mit Mittelbolzenaufhängung und radial angeordneten Stützbolzen
  • Fig 2 b wie 2 a, jedoch mit Stützring für die Vorspannfeder
  • Fig 3 a Druckplatte mit am Außenrand angreifenden Tragfedern und zentrischer Stützbüchse
  • Fig. 3 b Druckplatte wie 3 a mit parallel zur Maschinenachse in der Kalotte angeordneten Stützbolzen.
  • Fig. 4 a Druckplatte wie 3 a mit Anordnung eines mittigen Stützbolzens in der Kugelschale
  • Fig. 4 b Druckplatte wie 3a mit radial angeordneten Stützholzen in der Kugelschals
  • Fig. 5 Stutzbolzen mit hydraulischer Anpressung in die Kalotte eingebaut
  • Fig. 6 Stützbolzen mit hydraulischer Anpressung in die Kugelschale eingebaut
  • Fig. 7 Komplettes Stützelement zum Einbau in Kugelschale oder Kalotte
  • Fig. 8 Druckplatte mit hydraulischer Stützbüchse und hydraulischer Tragbüchse in der Kugelkalotte,
  • Fig. 9 a Druckplatte mit hydraulischer Stützbüchse und hydraulischer Tragbuchse in einer einseitigen Bohrung der Kugelkalotte,
  • Fig. 9 b Druckplatte mit hydraulischer Stützbüchse und Tragscheibe 41 in einer einseitigen Bohrung der Kugelkalotte;
  • Fig. 10 Druckplatte mit hydraulischer Stützbüchse und hydraulischer Tragbüchse in der Kugelschale,
  • Fig. 11 Druckplatte mit federbelasteter Stützbüchse und Hydraulik-Kolben am Tragbolzen,
  • Fig. 12 Druckplatte mit hydraulischer Tragbüchse und federbelasteter Stützbüchse in der Kugelkalotte,
  • Fig. 13 Druckplatte mit fedsrbelasteter Stützbüchse und mehreren Hydraulik-Kolben für den Tragholzen, in der Kugelschale angeordnet,
  • Fig. 14 Druckplatts mit kombinierter Stützbüchse-Tragbüchse in der Kugelschale angeordnet,
  • Fig. 15 Druckplatte mit kombinierter Stützbüchse-Tragbüchse in der Kugelschale angeordnet, mit Distanzbüchse.
Show it:
  • Fig. 1 a pressure plate with central pin suspension and central support sleeve
  • Fig 1 b pressure plate with central pin suspension and central support bushes for the recoil damping.
  • Fig. 2 a pressure plate with central pin suspension and radially arranged support pin
  • Fig. 2 b as 2 a, but with a support ring for the bias spring
  • Fig 3 a pressure plate with supporting springs acting on the outer edge and a central support sleeve
  • Fig. 3 b pressure plate as 3 a with parallel to the machine axis in the calotte arranged support bolts.
  • Fig. 4 a pressure plate as 3 a with the arrangement of a central support bolt in the spherical shell
  • Fig. 4 b pressure plate as 3a with radially arranged support beams in the ball scarves
  • Fig. 5 support bolts with hydraulic pressure installed in the calotte
  • Fig. 6 support bolt with hydraulic pressure installed in the ball socket
  • Fig. 7 Complete support element for installation in a spherical shell or spherical cap
  • 8 pressure plate with hydraulic support sleeve and hydraulic support sleeve in the spherical cap,
  • 9 a pressure plate with hydraulic support sleeve and hydraulic support bush in a one-sided bore of the spherical cap,
  • Fig. 9 b pressure plate with hydraulic support sleeve and support plate 41 in a one-sided bore of the spherical cap;
  • 10 pressure plate with hydraulic support sleeve and hydraulic support sleeve in the spherical shell,
  • 11 pressure plate with spring-loaded support sleeve and hydraulic piston on the support pin,
  • 12 pressure plate with hydraulic support sleeve and spring-loaded support sleeve in the spherical cap,
  • 13 pressure plate with spring-loaded support sleeve and several hydraulic pistons for the supporting beams, arranged in the spherical shell,
  • Fig. 14 pressure plate with combined support sleeve-carrying sleeve in the spherical shell arranged,
  • Fig. 15 pressure plate with combined support sleeve-carrying sleeve arranged in the spherical shell, with spacer sleeve.

Die Figur 1 a zeigt die Ausführung des Erfindugnsgegenstandes an einer durch einen Trag- oder Mittelbolzen 4 aufgehängten Druckplatte 3. In der Kugelkalotte 2 ist eine in Achsrichtung verschiebbere Stützbüchse 14 angeordnet, deren obere Stirnfläche 15 eine Oberfläche mit guten Gleiteigenschaften besitzt, z. B. Kunststoffbeschichtung. Durch Anspannen der Feder 5, durch die Mutter 6, ist die Stützbüchse mit anhängender Druckplatte soweit angehoben, daß die Stirnfläche 15 der Stützbüchse 14 an der Kugelschale 1 mit geringem Druck anliegt. Die Kalotte und Druckplatte liegen auf der Außenschulter 10 der Stützbüchse auf, die durch die Vorspannfeder 11 gegen den Tragbolzen 4 verspannt ist. Beim Ausrichten der Druckplatte wird diese nur durch die spherische Stirnfläche 15 der Stützbüchse 14 geführt. Beim Belasten wird die Kraft der Vorspannfeder 11 überwunden und die ganze restliche Kalotte mit rauherer Oberfläche legt sich gegen die Restkugelschale direkt an. Während der Einrichtphase liegt der Mittelpunkt A des Radius R der Kugelschale 1 in der Druckplattenebene 16, in der Arbeitsstellung liegt der Punkt A unterhalb der Druckplattenebene 16.FIG. 1 a shows the embodiment of the subject of the invention on a pressure plate 3 suspended by a support or center bolt 4. In the spherical cap 2 there is arranged a support sleeve 14 which can be displaced in the axial direction, the upper end face 15 of which has a surface with good sliding properties, e.g. B. plastic coating. By tightening the spring 5, by the nut 6, the support sleeve with attached pressure plate is raised so far that the end face 15 of the support sleeve 14 rests against the ball socket 1 with low pressure. The spherical cap and pressure plate rest on the outer shoulder 10 of the support sleeve, which is braced against the supporting bolt 4 by the biasing spring 11. When aligning the pressure plate, it is only guided through the spherical end face 15 of the support sleeve 14. When loaded, the force of the biasing spring 11 is overcome and the entire remaining calotte with a rougher surface lies directly against the remaining spherical shell. During the set-up phase, the center A of the radius R of the spherical shell 1 lies in the pressure plate plane 16, in the working position point A lies below the pressure plate plane 16.

Auf der Figur 1 b ist die gleiche Anordnung dargestellt, jedoch mit einer hydraulischen Rückstoßdämpfung. Die Ringkammer 24 ist während des Belastungsvorganges über die Druckleitung 22 mit einem Hydraulikspeicher verbunden, der ein konstantes Druckniveau besitzt. Damit ist folgendes machbar: das zur Dämpfung notwendige Druckniveau kann die Vorspannfeder 11 weiter spannen und damit die Kugelkalotte gegen die Kugelschale anhebend anpressen, wobei gleichzeitig die Stützbüchse 14 nach unten geschoben werden kann, bis sie unter der Kalottenoberfläche verschwindet, beim Einstellvorgäng kann die Ringkammer drucklos sein.The same arrangement is shown in FIG. 1b, but with hydraulic recoil damping. The annular chamber 24 is connected during the loading process via the pressure line 22 to a hydraulic accumulator which has a constant pressure level. The following is feasible: the pressure level required for damping can further tension the preload spring 11 and thus press the spherical cap against the spherical shell, while at the same time the support sleeve 14 can be pushed down until it disappears under the spherical surface, during the setting process the annular chamber can be depressurized be.

Bei der Ausführung nach Fig. 2 a ist die Kugelkalotte durch mindestens drei Stützbolzen 9 abgestützt und ausgerichtet, die in Bohrungen der Kalotte gleiten und mit Federn 11 vorgespannt sind. Die Federn stützen sich gegen die Druckplatte 3 ab.In the embodiment according to FIG. 2 a, the spherical cap is supported and aligned by at least three support bolts 9 which slide in bores of the spherical cap and are preloaded with springs 11. The springs are supported against the pressure plate 3.

Bei der Ausführung nach Fig. 2 b sind ähnliche Stützbolzen 9 vorhanden. Die Vorspannfeder 11 stützt sich gegen eine Endscheibe 12, z. B. einen Seeger-Ring ab. In die Stirnfläche der Stützbolzen sind Gleitstücke 25 aus einem leicht gleitenden Werkstoff eingesetzt. Auch hier verschiebt sich die Druckplattenebene 16 vom Mittelpunkt A des Schalenradius R bei Belastung nach oben. Die Auflagefläche des Tragbolzens 4 mit kleiner Kugelkalotte 8 gegen die kleine Kugelschale 7 ist an den Mittelpunkt der Kugelkalotte 2 herangeführt, um die Einstellkräfte für die Druckplatte 3 gering zu halten.Similar support bolts 9 are present in the embodiment according to FIG. 2 b. The bias spring 11 is supported against an end plate 12, for. B. from a Seeger ring. Sliders 25 made of a slightly sliding material are inserted into the end face of the support bolts. Here, too, the pressure plate plane 16 moves upward from the center A of the shell radius R under load. The contact surface of the supporting bolt 4 with a small spherical cap 8 against the small spherical shell 7 is brought up to the center of the spherical cap 2 in order to keep the setting forces for the pressure plate 3 low.

In der Fig. 3 a ist die Ausführung des Erfindungsgegenstandes an einer Druckplatte gezeigt, die an mindestens drei Federn 27 aufgehängt ist, die am äußeren Rand der Druckplatte 3 angreifen. In die Kugelkalotte 2 ist mittig eine Stützbüchse 14 eingebaut, deren Schulter durch die Feder 11 gegen die Schulter 10 der Bohrung in dar Kalotte 2 gedrückt wird.3 a shows the embodiment of the subject matter of the invention on a pressure plate which is suspended from at least three springs 27 which engage on the outer edge of the pressure plate 3. In the spherical cap 2, a support sleeve 14 is installed in the center, the shoulder of which is pressed by the spring 11 against the shoulder 10 of the bore in the spherical cap 2.

Bei der Ausführung nach Fig. 3b sind drei Stützbolzen 9 parallel zur Maschinenachse in der Kugelkalotte angeordnet.3b, three support bolts 9 are arranged parallel to the machine axis in the spherical cap.

Die Vorspannung der Feder 11 kann mit der Schraube eingestellt werden.The bias of the spring 11 can be adjusted with the screw.

Bei der Ausführung nach Fig. 4 a an einer ähnlich aufgehängten Druckplatte ist ein Stützbolzen 9, der in der mittigen Bohrung der Kugelschale 1 angeordnet ist und der durch die Feder 11 belastet ist, vorgesehen.4 a on a similarly suspended pressure plate, a support pin 9, which is arranged in the central bore of the spherical shell 1 and which is loaded by the spring 11, is provided.

Bei der Ausführung nach Fig. 4 b sind mindestsns drei Stütbolzen 9 in der Kugelschale radial angeordnet. Die nach oben hin offene Führungsbohrung ist durch eine Schraube 18 geschlossen, der zum Vorspannen der Feder 11 dient.In the embodiment according to FIG. 4 b, at least three support bolts 9 are arranged radially in the spherical shell. The guide bore, which is open at the top, is closed by a screw 18, which serves to bias the spring 11.

In einer weiteren Ausführungsform wird die Vorspannung für die Stützbolzen oder -büchsen hydraulisch aufgebaut.In a further embodiment, the pretension for the support bolts or bushes is built up hydraulically.

Nach der Ausführung der Fig. 5 ist dar Stützbolzen 9 mit einem Kolben 17 mit Dichtungsringen 17a verbunden, der in einer Bohrung der Kalotte gleitet. Die Rückseite der Bohrung ist mit Dichtringen durch einen dichtenden Stopfen 18 verschlossen. Das Drucköl wird durch die Leitung 23 zugeführt.5, the support pin 9 is connected to a piston 17 with sealing rings 17a, which slides in a bore in the calotte. The back of the bore is closed with sealing rings by a sealing plug 18. The pressure oil is supplied through line 23.

Nach der Ausfuhrung gemäß Fig. 6 ist das Stützelement in der Kugelschale 1 angeordnet, die Bohrung für die Führung von Stützbolzen 9 und Druckkolben 17 ist von oben her eingearbeitet und mit einem Gewindestopfen 18 mit Anschlußbohrung 22 für die Druckleitung verschlossen.6, the support element is arranged in the spherical shell 1, the bore for guiding the support bolt 9 and the pressure piston 17 is incorporated from above and closed with a threaded plug 18 with a connection bore 22 for the pressure line.

Bei der Ausführung nach Fig. 7 ist ein komplettes Stützelement mit Zylinder 19, Vorspannkolben 17 und Stützbolzen 9 in die Kugelschale eingesetzt.7, a complete support element with cylinder 19, biasing piston 17 and support pin 9 is inserted into the ball socket.

Das gleiche Element kann auch in die Kugelkalotte eingebaut sein. Anstelle des hydraulischen Druckes können diese kompletten Stützelemente mit Federvorspannung ausgerüstet sein.The same element can also be installed in the spherical cap. Instead of the hydraulic pressure, these complete support elements can be equipped with spring preload.

Die oben beschriebenen hydraulischen Stützelemente sind an einen Druckspeicher mit konstantem Öldruck angeschlossen oder sie werden von einer Speisepumpe versorgt. Die Speisepumpe fördert über einen Druckregler und ein dahinter geschaltetes Rückschlagventil in die Stützelemente. Ein Überdruckventil ist an das Stützelement angeschlagen.The hydraulic support elements described above are connected to a pressure accumulator with constant oil pressure or they are supplied by a feed pump. The feed pump feeds into the support elements via a pressure regulator and a check valve connected behind it. A pressure relief valve is attached to the support element.

Die Stirnflächen der Stützbüchsen bzw. Stützbolzen, die in die Kugelschale eingebaut sind, haben eine der Kugelschale angepaßte Form Fig. 2 a) oder sind kugelig (Fig. 3 b) ausgebildet.The end faces of the support bushes or support bolts, which are built into the spherical shell, have a shape adapted to the spherical shell, FIG. 2 a), or are spherical (FIG. 3 b).

Die Stirnfläche der Stützbolzen und -büchsen, die in der Kugelschale 1 eingebaut sind, haben eine der Kugelschale angepaßte Form oder eine kugelige bzw. eine ebene Form (Fig. 4b).The end face of the support bolts and bushings, which are installed in the spherical shell 1, have a shape adapted to the spherical shell or spherical or a flat shape (Fig. 4b).

Die Fig. 8 zeigt die Ausführung des Erfindungsgegenstandes an einer Anordnung, bei der zwei hydraulische Spanneinrichtungen benutzt werden, die in die Kugelkalotte 2 eingebaut sind, und die unabhängig voneinander arbeiten können. Bei dieser Anordnung kann auf eine Tragfeder z. B. Schraubenfeder verzichtet werden. Die Vorspannung zur Anlage der Stirnfläche 15 der Stützbuchse 14 gegen die Kugelschale 1 in der Einrichtsphase wird durch die Druckkammer 24 bewirkt. Die Anlage der Kugelkalotte nach Beendigung der Einstellphase an die Kugelschale wird durch die Tragbüchse 28 mit Druckkammer 24a bewirkt. Während des Einstellvorganges kann die Druckkammer 24a drucklos sein und die Druckkammer 24 kann mit einem Druck beaufschlagt werden der die Stützbüchse gerade an die Kugelschale anlegt oder mit einer höheren Vorspannung anpreßt. Nach Einstellen der Druckplatte auf die Neigung der Prüfkörperoberfläche kann der Prüfkörper und die Druckplatte durch den z. B. unten liegenden hydraulischen Antrieb der Maschine angehoben werden bis die Kugelkalotte an der Kugelschale anliegt und dann über die Ringkammer 24a eine Vorspannung erzeugt werden: es kann aber auch zunächst die Druckplatte über die Ringkammer 24a angehoben und gegen die Kugelschale gedrückt werden bevor der hydraulische Antrieb der Maschine die Probe anhebt. Während des Druckversuches kann die Ringkammer 24 drucklos sein, so daß die Stützbüchse hinter die Oberfläche der Kugelkalotte absinken kann.Fig. 8 shows the execution of the subject matter of an arrangement in which two hydraulic clamping devices are used, which are installed in the spherical cap 2, and which can work independently of each other. In this arrangement, a support spring z. B. coil spring can be dispensed with. The prestress for the abutment of the end face 15 of the support bush 14 against the spherical shell 1 in the set-up phase is brought about by the pressure chamber 24. The bearing of the spherical cap after the end of the adjustment phase on the spherical shell is brought about by the carrying sleeve 28 with the pressure chamber 24a. During the setting process, the pressure chamber 24a can be depressurized and the pressure chamber 24 can be subjected to a pressure which just applies the support sleeve to the ball socket or presses it with a higher prestress. After adjusting the pressure plate to the inclination of the test specimen surface, the test specimen and the pressure plate can be replaced by the z. B. The hydraulic drive of the machine located underneath can be raised until the spherical cap rests on the spherical shell and then a preload is generated via the annular chamber 24a: however, the pressure plate can also first be raised via the annular chamber 24a and pressed against the spherical shell before the hydraulic drive the machine lifts the sample. During the pressure test, the annular chamber 24 can be depressurized, so that the support sleeve can sink behind the surface of the spherical cap.

Nach einer anderen Ausführungsform kann die Ringkammer 24a unter einem gegebenenfalls konstanten hydraulischen Druck stehen und über die Stützbüchse als Stoßdämpfer beim Rückfedern der Druckplatte nach dem Probenbruch dienen.According to another embodiment, the annular chamber 24a can be under a possibly constant hydraulic pressure and can serve as a shock absorber via the support sleeve when the pressure plate springs back after the sample has broken.

Die Kugelkalotte selbst kann während des Versuches durch die Tragbüchse gegen die Kugelschale gedrückt werden, wodurch die übliche Vorspannfeder entfallen kann.The spherical cap itself can be pressed against the spherical shell by the carrying bushing during the test, whereby the usual preload spring can be omitted.

Fig. 9 a zeigt den Erfindungsgegenstand in einer Ausführungsform, bei der die Stüzbüchse 14 und die Tragbüchse 28 beide von einer Seite der in die zylindrische Bohrung der Kugelkalotte eingebracht werden können. Die Stützbüchse wird durch die Feder 11 gegen die Kugelschale gedrückt. Die Anpreßkraft wird durch die der Federkraft entgegenwirkende hydraulische Kraft in der Ringkammer 24 eingestellt. Nach der Einstellphase kann die Stützbüchse durch den hydraulischen Druck in Kammer 24 hinter die Kalotten-Oberfläche zurückgezogen werden. Die Tragbüchse 28 besitzt eine hydraulische Druckkammer 24a.9 a shows the subject of the invention in an embodiment in which the support sleeve 14 and the support sleeve 28 can both be introduced from one side into the cylindrical bore of the spherical cap. The support sleeve is pressed by the spring 11 against the spherical shell. The contact pressure is set in the annular chamber 24 by the hydraulic force counteracting the spring force. After the adjustment phase, the support sleeve can be retracted behind the calotte surface by the hydraulic pressure in chamber 24. The carrying sleeve 28 has a hydraulic pressure chamber 24a.

Fig 9 b zeigt den Erfindungsgegenstand in einer Ausführungsform, in der nur die Stützbüchse einen hydraulischen Antrieb mit Druckkammer 24 besitzt. In der Einstellphase wird nach Absenken des Druckes in der Kammer 24 die Feder 11 wirksam und die Stützbüchse tritt aus der Kugelkalotte heraus. Beim Übergang zum Versuch wird die Stützbüchse durch Druckanstieg in der Kammer 24 zunächst zurückgezogen, sodann setzt sich das verlängerte untere Teil der Stützbüchse als Hubbegrenzung 38 auf die Tragscheibe 41 ab, wobei der weitere Druckanstieg in der Kammer 24 die Kugelkalotte gegen die Kugelschale andrückt.9 b shows the subject matter of the invention in an embodiment in which only the support sleeve has a hydraulic drive with a pressure chamber 24. In the setting phase, after lowering the pressure in the chamber 24, the spring 11 takes effect and the support sleeve emerges from the spherical cap. At the transition to the experiment, the support sleeve is first pulled back by an increase in pressure in the chamber 24, then the elongated lower part of the support sleeve settles on the support plate 41 as a stroke limiter 38, the further increase in pressure in the chamber 24 pressing the spherical cap against the spherical shell.

Die Stützbüchse 21 und die Feder 11 können gegebenenfalls den Rückstoß bei der Rückfederung der Druckplatte dämpfen.The support sleeve 21 and the spring 11 can dampen the recoil when the pressure plate springs back.

In der Fig. 10 ist der Gegenstand der Erfindung in einer Ausführung gezeigt, bei der die hydraulische Stützbüchse 14 und die hydraulische Tragbüchse 28 auf der Seite der Kugelschale angeordnet ist, wobei die Funktion der Anordnung sinngemäß die gleiche ist, wie zur Fig. 1 beschrieben. Für die Aufhängung der Druckplatte kann zusätzlich eine Druckfeder 5 eingebaut sein.10 shows the subject matter of the invention in an embodiment in which the hydraulic support sleeve 14 and the hydraulic support sleeve 28 are arranged on the side of the spherical shell, the function of the arrangement correspondingly being the same as that described for FIG. 1 . A compression spring 5 can also be installed for the suspension of the pressure plate.

Bei der Ausführungsform nach Fig. 11 ist eine Vorspanneinrichtung mit einer Hydraulik, die andere mit einer Feder ausgerüstet, wobei der Tragbolzen mit dem Kolben 29 verbunden ist, der in der Zylinderbohrung 30 gleiten kann, und die Stützbüchse 14 von der Vorspannfeder 11 belastet wird. Beim Einstellvorgang wird der Druckraum 31 entlastet, wodurch die Stützbüchse 14 aus der Kugelkalotte heraustritt. Die Vorspannfeder 11 kann unabhängig von der Vorspannung im Tragbolzen dimensioniert werden. Oberhalb des Kolbens ist eine Kammer 32, die als Rückstoßdämpfe wirken kann, eingebaut, die mit einem Überdruckventil oder einem Druckakkumulator verbunden sein kann, zur Einstellung der Dämpfungswirkung. Der Zylinder mit Kolben 29 kann auch als separates Element auf der Oberfläche der Kugelschalentraverse angeordnet sein, womit ein hydraulischer Antrieb gegeben ist.In the embodiment according to FIG. 11, a pretensioning device is equipped with a hydraulic system, the other is equipped with a spring, the supporting bolt being connected to the piston 29, which can slide in the cylinder bore 30, and the supporting bush 14 is loaded by the pretensioning spring 11. During the adjustment process, the pressure chamber 31 is relieved, as a result of which the support sleeve 14 emerges from the spherical cap. The bias spring 11 can be dimensioned independently of the bias in the support bolt. A chamber 32, which can act as recoil vapors, is installed above the piston and can be connected to a pressure relief valve or a pressure accumulator for adjusting the damping effect. The cylinder with piston 29 can also be arranged as a separate element on the surface of the spherical shell cross member, which provides a hydraulic drive.

In der Fig. 12 ist, eine Anordnung mit, Stütztbüchse 14, Spannfeder 11 und hydraulischer Tragbüchse 28 dargestellt. In der Einstellphase ist die Druckkammer 24a entlastet, wodurch die Stützbüchse allein zur Anlage kommt.FIG. 12 shows an arrangement with a support sleeve 14, tension spring 11 and hydraulic support sleeve 28. In the setting phase, the pressure chamber 24a is relieved, as a result of which the support sleeve comes into contact alone.

Bei der Ausführungsform nach Fig. 13 sind mindestens zwei Zylinderbohrungen 34 mit Plunscherkolben 33 vorhanden, die über eine Tragscheibe 39 den Tragbolzen 4 anheben können. Die Stützbüchse 14 wird mit der Feder 11 belastet. Die Plunscherkolben können auch in getrennten Zylindern angeordnet werden, die auf der Kugelschalentraverse angsordnet sind.In the embodiment according to FIG. 13, there are at least two cylinder bores 34 with plummer pistons 33, which can lift the supporting bolt 4 via a supporting disk 39. The support sleeve 14 is loaded with the spring 11. The plunger pistons can also be arranged in separate cylinders which are arranged on the spherical shell cross member.

Bei der Ausführungsform nach Fig. 14 ist die Stützbüchse 14 und die Tragbüchse 28 in einem Bauteil vereinigt (sogenannte Stütz-Tragbüchse). In der Einrichtephase kann die Druckkammer 24a drucklos sein, wodurch die Stütz-Tragbüchse 14/28 auf der Schulter 36 der Kugelschale aufliegt. In der Versuchsphase wird die Stütz-Tragbüchse durch Druck in der Kammer 24 a angehoben, worauf sich die Stütz-Tragbüchse gegen die Schulter 35 des Tragbolzens 4 anlegt und die Vorspannung für diesen übernimmt.In the embodiment according to FIG. 14, the support sleeve 14 and the support sleeve 28 are combined in one component (so-called support support sleeve). In the setup phase, the pressure chamber 24a can be depressurized, as a result of which the support carrying sleeve 14/28 rests on the shoulder 36 of the spherical shell. In the test phase, the support liner is raised by pressure in the chamber 24 a, whereupon the support liner rests against the shoulder 35 of the support bolt 4 and takes over the prestressing for it.

Der Hub der Stütz-Tragbüchse 14/28 kann so ausgelegt sein, daß die Stütz-Tragbüchse sich erst dann gegen die Schulter 35 des Tragbolzens 4 anlegt, wenn die Stütz-Tragbüchse hinter die Oberfläche der Kugelschale zurückgetreten ist.The stroke of the support bushing 14/28 can be designed so that the support bushing only rests against the shoulder 35 of the support bolt 4 when the support bushing has withdrawn behind the surface of the spherical shell.

In der Fig. 15 ist eine Ausführungsform gezeigt, bei der anstelle der Schulter 35 der Abb. 14 eine Distanzbüchse 37 verwendet wird.15 shows an embodiment in which a spacer sleeve 37 is used instead of the shoulder 35 of FIG. 14.

An die Stelle der Distanzbüchse kann auch eine Feder treten.A spring can also replace the spacer sleeve.

Die Zeichnungen zeigen beispielhafte Kombinationen und Anordnungen vonThe drawings show exemplary combinations and arrangements of

Stützbüchse und Tragbüchse.Support sleeve and carrying sleeve.

Die Einstellung der Spann- oder Verspann Kräfte ist wie folgt möglich:

  • 1. Eine oder beide Spannkräfte werden durch die Art der Konstruktion unveränderbar festgelegt, gegebenenfalls ist ihr Verhältnis vor oder während des Versuchs veränderbar.
  • 2. Eine oder beide Spannkräfte werden vor dem Versuch eingestellt.
  • 3. Eine oder beide Spannkräfte können während des Versuchs geregelt werden.
The setting of the clamping or bracing forces is possible as follows:
  • 1. One or both clamping forces are fixed unchangeably by the type of construction, if necessary their ratio can be changed before or during the test.
  • 2. One or both clamping forces are set before the experiment.
  • 3. One or both clamping forces can be regulated during the test.

Durch das Verfahren und die Vorrichtung nach der Erfindung werden eindeutige und reproduzierbare Prüfbedingungen für die Durchführung von Druckversuchen erhalten, da sowohl die leichte Einstellbarkeit der Druckplattenneigung in der Einstellphase verwirklicht ist, wie auch die Verhinderung von Relativverschiebungen der Kalotte und Schale während des eigentlichen Druckversuches. Zur Erreichung dieses Zieles werden nur wenige zusätzliche, einfache Maschinenelemente benötigt, so daß eine wirtschaftliche Herstellung der Vorrichtung gegeben ist.

Figure imgb0001
Figure imgb0002
The method and the device according to the invention provide clear and reproducible test conditions for carrying out printing tests, since both the easy adjustability of the printing plate inclination is achieved in the setting phase and the prevention of relative displacements of the calotte and shell during the actual printing test. To achieve this goal, only a few additional, simple machine elements are required, so that the device can be produced economically.
Figure imgb0001
Figure imgb0002

Claims (17)

1. Method for the mounting and adjustment of pressure plates in materials testing machines, which have a pressure plate with a spherical cup, a spherical shell which is connectable with the testing machine for receiving the spherical cup, and connecting elements for connecting the spherical cup and the spherical shell, the adjustment of the pressure plate to the inclination of the pressure surface of the test piece being effected first and thereafter, on loading, a relative movement between the spherical cup and spherical shell being prevented, characterised in that
- for the almost force-free adjustment of the pressure plate to the inclination of the pressure surface of the test piece which is brought against it whilst maintaining a centering of the spherical cup to the spherical shell, a first pair of contact surfaces is brought into effect, which pair consists of spherical shell and spherical cup elements which can be supported against each other and which are arranged concentrically to the spherical shell axis, and which pair forms a contact surface with slight friction,
- and that thereafter, on loading, a second pair of contact surfaces, consisting of a spherical cup and spherical shell, is brought into effect, the second contact surfaces having a high coefficient of friction, so that on resting the spherical cup against the spherical shell, a relative movement between the spherical cup and the spherical shell is prevented by frictional connection or respectively static friction.
2. Method according to Claim 1, characterised in that on the adjustment of the pressure plate, the central point of the spherical shell (A) lies in the pressure surface plane of the pressure plate and on loading the central point (A) lies beneath the pressure surface plane.
3. Method according to Claim 1 or 2, characterised in that the resistance of the pressure plate with respect to an alteration to its inclination is adjusted in that an initial stressing force acting on the contact surfaces and/or the ratio of the initial stressing forces acting on the contact surfaces is adjusted.
4. Method according to Claim 3, characterised in that at least one initial stressing force is altered before and/or during the test.
5. Method according to Claim 3 or 4, characterised in that the initial stressing force is produced or altered mechanically.
6. Method according to Claim 3 or 4, characterised in that the initial stressing force is produced or altered hydraulically.
7. Device for the mounting and adjustment of pressure plates in materials testing machines, which has a pressure plate (3) with a spherical cup (2), a spherical shell (1) which is connectable with the testing machine for receiving the spherical cup (2), and connecting elements for connecting the spherical cup and spherical shell, for carrying out the method according to one of Claims 1 to 6, characterised in that in the spherical shell (1) or in the spherical cup (2) at least one support element (9,14), which is movable with respect to the bearing surface of the spherical cup (2) or respectively with respect to the spherical shell (1), is arranged to support the spherical cup (2) on the spherical shell (1), that the surface of the support element which comes into contact with the spherical shell (1) or respectively spherical cup (2) has good sliding properties and that the support element for supporting the spherical cup (2) on the spherical shell (1) can be acted upon by springs (11) or hydraulically via cylinder/piston arrangements.
8. Device according to Claim 7, characterised in that the support elements are constructed as centrally arranged support sleeve (14) or in the form of at least three support pins (9) which are distributed over the surface of the spherical shell (1) or respectively the spherical cup (2).
9. Device according to Claim 8 with a connecting element constructed as a carrier pin, characterised in that the carrier pin (4) is arranged in the spherical shell (1) and is passed through a central opening of the support sleeve (14), that the support sleeve (14) rests with an inner shoulder on a collar of the carrier pin, the support between the collar of the carrier pin (4) and the support sleeve (14) taking place via spherical surfaces (20), that the support sleeve (14) has an outer shoulder (10), against which the spherical cup (2) can be placed and that a prestressing spring (11) is provided, with which the support sleeve (14) and the spherical cup (2) can be braced against each other such that the contact surface of the support sleeve projects beyond the contact surface of the spherical cup (2).
10. Device according to Claim 9, characterised in that an annular chamber (24), which is formed between the outer shoulder (10) of the axially movable support sleeve (14) and the spherical cup (2), can be acted upon by a pressure medium.
11. Device according to Claim 8, with a connecting element constructed as a carrier pin, characterised in that the support pins (9) have a collar (13) and are supported by a spring (11) against the spherical cup (2) and that the spherical cup (2) is supported against spherical surfaces on a collar of the carrier pin (4).
12. Device according to Claim 8, characterised in that the support elements consist of cylinders (19), pistons (17) with sealing rings (17a), support pins (9) and threaded plugs (18) with sealing rings (18a).
13. Device according to Claim 7 with a connecting element constructed as a carrier pin, characterised in that in the spherical cup (2) or in the spherical shell (1) a support sleeve (14) and a carrier sleeve (28) are arranged axially movably and coaxially such that they are penetrated centrally by the carrier pin (4), that the support sleeve (14) and carrier sleeve (28) have an outer shoulder, that the outer shoulders cooperate with steps in the spherical cup (2) or spherical shell (1) and thereby form annular chambers (24, 24a) which can be acted upon hydraulically, that the outer shoulders and steps are arranged such that when the annular chambers (24, 24a) are acted upon, the support sleeve (14) and the carrier sleeve (28) move away from each other, that the carrier sleeve (28) is supported on a collar on one end of the carrier pin (4) and the carrier pin (4) supports itself on its other end on the spherical shell (1), or respectively that the carrier pin (4) carries the spherical cup (2) on one end through a collar with spherical contact surfaces and supports itself on the other end on the carrier sleeve (28).
14. Device according to Claim 7 with a connecting element constructed as a carrier pin, characterised in that in the spherical cup (2) a support sleeve (14) and a carrier sleeve (28) are arranged axially movably and coaxially such that they are penetrated centrally by the carrier pin (4), that the support sleeve (14) and carrier sleeve (28) have an outer shoulder, that the outer shoulders cooperate withsteps in the spherical cup (2) and thereby form annular chambers (24, 24a) which can be acted upon hydraulically, that the outer shoulders and steps are arranged such that when the annular chambers (24, 24a) are acted upon, the support sleeve (14) and carrier sleeve (28) move in the same direction and that the carrier pin (4) is supported elastically against the spherical shell (1) and carries the carrier sleeve (28) on its other end on a collar via a spherical surface, the prestressing spring (11) being arranged between the support sleeve (14) and carrier sleeve (28).
15. Device according to Claim 8 with a connecting element constructed as a carrier pin, characterised in that the carrier pin (4) acts on a carrier disc (41) in the spherical cup (2) on spherical annular surfaces, against which disc the prestressing spring (11) also supports itself for action upon the support sleeve (14) and that the carrier pin (4) in the spherical shell (1) is connected to a piston/cylinder arrangement (29, 30) which is able to be acted upon hydraulically.
16. Device according to Claim 8 with a connecting eelement constructed as a carrier pin, characterised in that the carrier pin (4) in the spherical cup (2) acts via a collar on spherical surfaces on an axially movable carrier sleeve (28) which is arranged coaxially to the carrier pin (4), on which carrier sleeve the prestressing spring (11) for the support sleeve (14) is also supported and that the carrier sleeve (28) has an outer shoulder, which with a step in the spherical cup (2) forms an annular chamber (24a) which can be acted upon hydraulically.
17. Device according to Claim 8 with a connecting element constructed as a carrier pin, characterised in that the spherical cup (2) is supported on spherical surfaces on a collar of the carrier pin (4), that in the spherical shell (1) a combined support/carrier sleeve (14, 28) is arranged, which has an outer shoulder and with a shoulder (36) in the spherical shell (1) forms an annular chamber (24a) which can be acted upon hydraulically and that the carrier pin (4) is supported via a prestressing spring (11) on the support/carrier sleeve (14, 28).
EP19820106183 1981-07-17 1982-07-10 Method and apparatus for positioning the pressure plate in material testing devices Expired EP0070480B1 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
DE3128394 1981-07-17
DE19813128394 DE3128394C2 (en) 1981-07-17 1981-07-17 Method and device for the adjustable mounting of printing plates in materials testing machines
DE19823201389 DE3201389A1 (en) 1982-01-19 1982-01-19 Process and device for mounting pressure plates in material-testing machines
DE3201389 1982-01-19

Publications (3)

Publication Number Publication Date
EP0070480A2 EP0070480A2 (en) 1983-01-26
EP0070480A3 EP0070480A3 (en) 1984-06-13
EP0070480B1 true EP0070480B1 (en) 1987-09-02

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EP19820106183 Expired EP0070480B1 (en) 1981-07-17 1982-07-10 Method and apparatus for positioning the pressure plate in material testing devices

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Cited By (1)

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Publication number Priority date Publication date Assignee Title
CN103712851A (en) * 2013-12-20 2014-04-09 浙江大学 High-pressure hydrogen environment fatigue test clamp for material testing machine

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3316218C2 (en) * 1983-05-04 1994-06-01 Roell & Korthaus Mfl Gmbh & Co Spherical bearing pressure plate for material testing machines
FR2686977A1 (en) * 1992-02-04 1993-08-06 Commissariat Energie Atomique Device for creep testing a sample
DE4204589A1 (en) * 1992-02-15 1993-08-19 Mtu Muenchen Gmbh MATERIALS TEST DEVICE FOR TENSION OR PRESSURE TESTS
US20090235755A1 (en) * 2008-03-18 2009-09-24 Illinois Tool Works Inc. Rotating dovetail connection for materials testing
CN104316396B (en) * 2014-10-30 2016-10-12 凯尔测控试验系统(天津)有限公司 A kind of XYZ tri-shaft assignment adjusting means of mechanics machine
CN109870350B (en) * 2019-03-29 2023-10-27 中国矿业大学 Liquid leakage prevention high-temperature high-pressure hydraulic fracturing system and test method
CN111207277A (en) * 2020-03-09 2020-05-29 浙江中信检测有限公司 Field Surveying and Mapping System for Engineering Surveying and Mapping
CN112362481B (en) * 2020-10-27 2022-06-14 哈尔滨工程大学 Pressure-resistant shell compression-resistant testing device

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB763374A (en) * 1954-05-08 1956-12-12 Saml Denison & Son Ltd Improved method and means for testing the tensile or compressive properties of materials
GB1244173A (en) * 1968-01-26 1971-08-25 Saml Denison & Son Ltd Improvements relating to physical testing machines

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103712851A (en) * 2013-12-20 2014-04-09 浙江大学 High-pressure hydrogen environment fatigue test clamp for material testing machine
CN103712851B (en) * 2013-12-20 2016-01-20 浙江大学 High pressure hydrogen environment Material Testing Machine fatigue test clamper

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EP0070480A2 (en) 1983-01-26
EP0070480A3 (en) 1984-06-13

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